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卫星编队自主队形控制 被引量：3

Autonomous Formation Control for Spacecraft Formation Flying
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摘要 为了实现高精度的卫星编队飞行,提出了一种基于主从结构的协同控制方法-自主队形控制法。在主星变轨的过程中,卫星编队的队形可以保持不变。文中介绍了该控制法的设计思想,给出了实现结构图,并详细的分析了该方法优缺点。通过算例验证了自主队形控制法的可行性。 This paper considers the precise control of formation control in Earth-orbiting spacecraft formation flying(SFF).An autonomous formation control scheme based on the leader-follower approach is developed.The main advantage of this scheme is that the followers can autonomously keep the internal geometry intact while driving the leader to desired orbit.The coordinated control architecture is provided.The advantages and drawbacks of this scheme are discussed in detail.To determine the feasibility of this scheme...
作者 刘辉 李俊峰
机构地区 清华大学航天航空系
出处 《宇航学报》 EI CAS CSCD 北大核心 2007年第5期1138-1141,共4页 Journal of Astronautics
关键词 编队飞行 队形控制 协同控制 Spacecraft formation flying Autonomous formation control Coordinated control
分类号 V448.2 [航空宇航科学与技术—飞行器设计]
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参考文献8

  • 1[1]Scharf D P,Hadaegh F Y,Ploen S R.A survey of spacecraft formation flying Guidance and control (Part Ⅱ):control[C]//Proceeding of the 2004 American control conference,Boston,2004
  • 2[2]Redding D C,Adams N J,Kubiak E T.Linear-quadratic stationkeeping for the STS orbiter[J].J.of Guidance,Control,and Dynamics,1989,12(2):248-255
  • 3[3]Vikram Kapila,Andrew G,Sparks,James M,Buffington,et al.Spacecraft formation flying:Dynamic and control[J].J.Guidance,2000,23(3):561-564
  • 4[4]Marcio S,de Queiroz,Vikram Kapilar,Qiguo Yan.Adaptive nonlinear control of multiple spacecraft formation flying[J].J.Guidance,Control,and Dynamics,2000,23(3):385-390
  • 5[5]Yeh His-Han,Nelson E,Sparks A.Nonlinear tracking control for satellite formations[J].J.Guidance,Control,and Dynamics,2002,25(2):376-386
  • 6[6]Wei Kang,Andy Sparks,Siva Banda.Coordinated control of multisatellite systems[J].J.Guidance,Control,and Dynamics,2001,24(2):360-368
  • 7[7]Massey T,ShtesselY.Continuous traditional and high-order sliding modes for satellite formation control[J].J.Guidance,Control,and Dynamics,2005,28(4):826-831
  • 8[8]Mohammed J L.SpaceCAPS:Automated mission planning for the TechSat21 formation-flying cluster experiment.http://www.stottlerhenke.com/papers/FLAIRS_ 2002 _ Spacecaps.pdf,2002

同被引文献42

  • 1孟云鹤,韩宏伟,戴金海.近地轨道航天器编队构形重构的一种四冲量控制方法[J].宇航学报,2008,29(2):505-510. 被引量：8
  • 2刘辉,李俊峰.卫星编队飞行的协同控制[J].清华大学学报（自然科学版）,2006,46(11):1922-1925. 被引量：7
  • 3Yeh H H, Nelson E, Sparks A. Nonlinear tracking control for satellite formations [ J ]. Journal of Guidance, Control, and Dynamics, 2002, 25 (2) : 376-386.
  • 4Massey T, Shtessel Y. Continuous traditional and high- order sliding modes for satellite formation control [ J ]. Journal of Guidance, Control, and Dynamics, 2005, 28 (4) : 826-831.
  • 5Yeh H H, Nelson E, Sparks A. Nonlinear tracking control for satellite formations [J]. Journal of Guidance, Control, and Dynamics, 2002, 25 (2) : 376-386.
  • 6Massey T, Shtessel Y. Continuous traditional and high- order sliding modes for satellite formation control [J]. Journal of Guidance, Control, and Dynamics, 2005, 28 (4) : 826-831.
  • 7Liu H, Li J,Baoyin H X. Sliding mode control for low-thrust earth-orbiting spacecraft formation maneuvering [ J]. Aerspace Science and Technology, 2006, 10 (7) : 636 -643.
  • 8Yu S H, Yu X H. Continuous finite-time control for robotic manipulators with terminal sliding mode[J]. Automatica, 2005, 41(11) : 1957-1964.
  • 9Yu X, Man Z. Variable structure systems with terminal sliding modes[ M]. Lecture Notes in Control and Infor- mation Sciences, Springer-Verlag, 2002,109-128.
  • 10Yu X, Wu Y, Man Z. On global stabilization of nonlinear dynamical systems [ M ]. Lecture Notes in Control and Information Sciences, Springer-Verlag, 1999, 109- 122.

引证文献3

二级引证文献4

宇航学报
2007年 第5期

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